Stagnation point reverse flow combustor for a combustion system

F - Mech Eng,Light,Heat,Weapons – 23 – C

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F23C 9/00 (2006.01)

Patent

CA 2574091

A combustor assembly includes a combustor vessel having a wall, a proximate end defining an opening and a closed distal end opposite said proximate end. A manifold is carried by the proximate end. The manifold defines a combustion products exit. The combustion products exit being axially aligned with a portion of the closed distal end. A plurality of combustible reactant ports is carried by the manifold for directing combustible reactants into the combustion vessel from the region of the proximate end towards the closed distal end.

La présente invention concerne un ensemble chambre de combustion comprenant une chambre de combustion pourvue d'une paroi, d'une extrémité proximale définissant une ouverture, et d'une extrémité distale fermée à l'opposé de ladite extrémité proximale. Une rampe de distribution est supportée par l'extrémité proximale. Cette rampe de distribution définit une sortie des produits de combustion dans l'alignement d'une partie de l'extrémité distale fermée. Une pluralité d'orifices à réactant combustible est supportée par la rampe de distribution de façon à diriger ces réactants combustibles dans la chambre de combustion depuis la zone de l'extrémité proximale en direction de l'extrémité distale fermée.

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